DELTA 1 R/B, 2661

Orbit data source: Space-Track

DELTA 1 R/B, 2661 is space debris in SSO originally from a launch on Thu, 26 Jan 1967 UTC launched from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
2661, 1967-006B
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
33 kg wet, 33 kg dry
Launch date (UTC)
1967-01-26 (59 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.8 m
Radar Cross Section
0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 DELTA 1 R/B
1 02661U 67006B   25260.82682451 -.00000045  00000-0  18848-4 0  9998
2 02661 101.9591 326.3325 0064701 230.0101 242.0687 12.68015380713635
Epoch: 2025-09-17T19:50Z
TLE epoch observation values (Epoch: 2025-09-17T19:50:37.637Z)
Latitude
65.6842°
Longitude
-120.51724°
Altitude
1,425.004 km
Speed
7.143 km/s
True Right ascension
11h 36m 32s
True Declination
65° 33' 57"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
22:13:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,437.815 km
Perigee altitude
1,337.326 km
Semi-major axis
7,765.708 km
Eccentricity
0.00647
Inclination
101.9591°
RAAN
326.3325°
Arg. of periapsis
230.0101°
True anomaly
241.41614°
Mean anomaly
242.0687°
Eccentric anomaly
241.74217°
Mean motion
3.17155 °/min
Orbital period
113.51 mins
BSTAR
0.000018848
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Other satellites on launch #6 in the year 1967 (1967-01-26 UTC)

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